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[an error occurred while processing this directive]收稿日期: 2011-10-08
网络出版日期: 2025-05-29
基金资助
中央高校基本科研业务费专项资金(HEUCF100201)
The Numerical Simulation of Aluminum Droplet Combustion in Multi-phase Fluid
Received date: 2011-10-08
Online published: 2025-05-29
刘丛林 , 郜冶 , 贺征 . 铝颗粒在多相流中燃烧的数值模拟[J]. 弹箭与制导学报, 2012 , 32(3) : 118 -120,124 . DOI: 10.15892/j.cnki.djzdxb.2012.03.029
The aluminum droplet's burning detail is important for propellant capability. Based on Fick's first law and Fourier law, the mass and energy diffusion process between gases produced by burning aluminum droplet was computed. Following the track of the intermediate product, the development of droplet's size, component, and combustion efficiency were studied. Results show that in early process, the reaction is more intense. After 60 ms, the burning becomes placid. Finally, about 20% of the droplet surface is covered by the oxide cap.
Key words: solid rocket propellant; aluminum droplet; transient combustion; oxide cap
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